Source Code
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These source-code files are part of a reconstructed copy of Comanche 051, the
original release of the Apollo 11 Command Module (CM) Apollo Guidance Computer
(AGC) software.
The reconstruction began with source code of Comanche 055 previously transcribed
from a digitized copy of that program. The code was then updated by undoing
changes related to the R-2 lunar potential model, using hints from program
comments and change-indicating asterisks in the Comanche 055 listing as a guide.
The reconstruction was verified by matching memory-bank checksums to those listed
in drawing 2021153D. Note that page numbers in the reconstructed code match those
on the Comanche 055 printout, although the added code would likely have changed page
numbers for a real Comanche 051 listing.
Comments from the original source code are prefixed with a single '#' symbol,
whereas comments added later are prefixed by "##" or "###". Report any errors
noted by creating an
issue report at the Virtual AGC
project's GitHub repository.
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012124,000002: ## Copyright: Public domain.
012125,000003: ## Filename: CSM_GEOMETRY.agc
012126,000004: ## Purpose: A section of Comanche revision 051.
012127,000005: ## It is part of the reconstructed source code for the
012128,000006: ## original release of the flight software for the Command
012129,000007: ## Module's (CM) Apollo Guidance Computer (AGC) for Apollo 11.
012130,000008: ## The code has been recreated from a copy of Comanche 055. It
012131,000009: ## has been adapted such that the resulting bugger words
012132,000010: ## exactly match those specified for Comanche 51 in NASA drawing
012133,000011: ## 2021153D, which gives relatively high confidence that the
012134,000012: ## reconstruction is correct.
012135,000013: ## Reference: pp. 285-296
012136,000014: ## Assembler: yaYUL
012137,000015: ## Contact: Ron Burkey <info@sandroid.org>.
012138,000016: ## Website: www.ibiblio.org/apollo/index.html
012139,000017: ## Mod history: 2019-07-30 MAS Created from Comanche 55.
012140,000018:
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Page 285
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012142,000020: 22,2000 BANK 22
012143,000021: 23,2000 SETLOC COMGEOM1
012144,000022: 23,2000 BANK
012145,000023:
012146,000024: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012147,000025: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
012148,000026:
012149,000027: # THE INPUTS ARE 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012150,000028: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012151,000029: # JOB VAC AREA.
012152,000030:
012153,000031: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012154,000032: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012155,000033:
012156,000034: 23,2000 COUNT 23/GEOM
012157,000035:
012158,000036: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012159,000037: 23,2001 00006 5,1 # TRUNNION = TA
012160,000038: 23,2002 45513 CDULOGIC
012161,000039: 23,2003 41434 RTB PUSH
012162,000040: 23,2004 46027 SXTLOGIC
012163,000041: 23,2005 72556 SIN SL1
012164,000042: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012165,000043: 23,2007 00004 3,1 # SHAFT = SA
012166,000044: 23,2010 41434 RTB PUSH # PD4 = SA
012167,000045: 23,2011 45513 CDULOGIC
012168,000046:
012169,000047: 23,2012 41346 COS DMP
012170,000048: 23,2013 00003 2
012171,000049: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012172,000050:
012173,000051: 23,2015 41356 SIN DMP
012174,000052: 23,2016 77626 STADR
012175,000053: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012176,000054:
012177,000055: 23,2020 77746 COS
012178,000056: 23,2021 24045 STOVL STARM +4
012179,000057: 23,2022 00041 STARM # STARM = 32D
012180,000058: 23,2023 76521 MXV VSL1
012181,000059: 23,2024 06302 NB1NB2
012182,000060: 23,2025 00041 STORE 32D
012183,000061: 23,2026 77616 RVQ
012184,000062:
012185,000063: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012186,000064: 23,2030 26154 ADS MPAC
012187,000065: 23,2031 35003 CAF QUARTER
012188,000066: 23,2032 07256 TC SHORTMP
012189,000067: 23,2033 06030 TC DANZIG
012190,000068:
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012192,000070: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012193,000071: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012194,000072: # ERENCED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012195,000073: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012196,000074:
012197,000075: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012198,000076: # INPUT AS *SMNB*, I.E. SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012199,000077: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012200,000078:
012201,000079: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012202,000080: # EQUAL TO ZERO).
012203,000081:
012204,000082: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
012205,000083: 23,2035 00034 28D
012206,000084: 23,2036 02766 STAR
012207,000085: 23,2037 77624 CALL
012208,000086: 23,2040 47644 *SMNB*
012209,000087: 23,2041 76521 MXV VSL1
012210,000088: 23,2042 06260 NB2NB1
012211,000089: 23,2043 26766 STOVL STAR
012212,000090: 23,2044 15333 HIUNITX
012213,000091: 23,2045 26555 STOVL XNB1
012214,000092: 23,2046 15331 HIUNITY
012215,000093: 23,2047 26563 STOVL YNB1
012216,000094: 23,2050 15327 HIUNITZ
012217,000095: 23,2051 36571 STCALL ZNB1
012218,000096: 23,2052 46076 SXTANG1
012219,000097:
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012221,000099: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012222,000100: # SIGHT LIES ALONG THE STAR VECTOR.
012223,000101:
012224,000102: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012225,000103: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB,AND
012226,000104: # ZNB.
012227,000105:
012228,000106: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012229,000107: # EQUAL TO ZERO).
012230,000108:
012231,000109: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012232,000110: 23,2054 00034 28D
012233,000111: 23,2055 45662 TRANSP1 # EREF WRT NB2
012234,000112: 23,2056 64375 VLOAD MXV
012235,000113: 23,2057 02714 XNB
012236,000114: 23,2060 06260 NB2NB1
012237,000115: 23,2061 77772 VSL1
012238,000116: 23,2062 26555 STOVL XNB1
012239,000117: 23,2063 02722 YNB
012240,000118: 23,2064 76521 MXV VSL1
012241,000119: 23,2065 06260 NB2NB1
012242,000120: 23,2066 26563 STOVL YNB1
012243,000121: 23,2067 02730 ZNB
012244,000122: 23,2070 76521 MXV VSL1
012245,000123: 23,2071 06260 NB2NB1
012246,000124: 23,2072 02571 STORE ZNB1
012247,000125:
012248,000126: 23,2073 47034 RTB RTB
012249,000127: 23,2074 45662 TRANSP1
012250,000128: 23,2075 45676 TRANSP2
012251,000129:
012252,000130: 23,2076 47375 SXTANG1 VLOAD VXV
012253,000131: 23,2077 02571 ZNB1
012254,000132: 23,2100 02766 STAR
012255,000133: 23,2101 77600 BOV
012256,000134: 23,2102 46103 +1
012257,000135: 23,2103 40056 UNIT BOV
012258,000136: 23,2104 46145 ZNB=S1
012259,000137: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012260,000138:
012261,000139: 23,2106 57441 DOT DCOMP
012262,000140: 23,2107 02555 XNB1
012263,000141: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012264,000142: 23,2111 00027 PDA
012265,000143:
012266,000144: 23,2112 77641 DOT
012267,000145: 23,2113 02563 YNB1
012268,000146: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012269,000147: 23,2115 47256 ARCTRIG
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012271,000149: 23,2116 77634 RTB
012272,000150: 23,2117 45546 1STO2S
012273,000151: 23,2120 26774 STOVL SAC
012274,000152: 23,2121 02766 STAR
012275,000153: 23,2122 77600 BOV
012276,000154: 23,2123 46124 +1
012277,000155: 23,2124 72441 DOT SL1
012278,000156: 23,2125 02571 ZNB1
012279,000157: 23,2126 77726 ACOS
012280,000158: 23,2127 62440 BMN SL2
012281,000159: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012282,000160: 23,2131 45200 BOV DSU
012283,000161: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012284,000162: 23,2133 06331 20DEG-
012285,000163: 23,2134 77634 RTB
012286,000164: 23,2135 45546 1STO2S
012287,000165: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012288,000166: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012289,000167: 23,2140 01630 CULTFLAG
012290,000168: 23,2141 00034 28D
012291,000169: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012292,000170: 23,2143 01430 CULTFLAG
012293,000171: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012294,000172: 23,2145 77745 ZNB=S1 DLOAD
012295,000173: 23,2146 06325 270DEG
012296,000174: 23,2147 16774 STODL SAC
012297,000175: 23,2150 06327 20DEGS-
012298,000176: 23,2151 02776 STORE PAC
012299,000177: 23,2152 77614 CLRGO
012300,000178: 23,2153 01630 CULTFLAG
012301,000179: 23,2154 00034 28D
012302,000180:
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012304,000182: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012305,000183: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012306,000184: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012307,000185: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012308,000186: # OTHER VEHICLES COMPUTER.
012309,000187:
012310,000188: # INPUT
012311,000189: # STATE VECTOR IN TEMPORARY STORAGE AREA
012312,000190: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012313,000191: # SET X2 TO +2
012314,000192: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012315,000193: # SET X2 TO 0
012316,000194:
012317,000195: # OUTPUT
012318,000196: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012319,000197: # OR
012320,000198: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012321,000199:
012322,000200: 23,2155 BANK 23
012323,000201: 10,2000 SETLOC COMGEOM2
012324,000202: 10,2000 BANK
012325,000203: 10,2237 COUNT 10/GEOM
012326,000204: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012327,000205: 10,2240 04756 AVEMIDSW
012328,000206: 10,2241 20242 +1
012329,000207: 10,2242 53775 VLOAD VSL*
012330,000208: 10,2243 01521 TDELTAV
012331,000209: 10,2244 57605 0 -7,2
012332,000210: 10,2245 53655 VAD VSL*
012333,000211: 10,2246 01535 RCV
012334,000212: 10,2247 57576 0,2
012335,000213: 10,2250 25171 STOVL RN
012336,000214: 10,2251 01527 TNUV
012337,000215: 10,2252 53257 VSL* VAD
012338,000216: 10,2253 57602 0 -4,2
012339,000217: 10,2254 01543 VCV
012340,000218: 10,2255 77657 VSL*
012341,000219: 10,2256 57576 0,2
012342,000220: 10,2257 15177 STODL VN
012343,000221: 10,2260 01517 TET
012344,000222: 10,2261 01205 STORE PIPTIME
012345,000223: 10,2262 77616 RVQ
012346,000224:
012347,000225: 10,2263 53775 SVDWN2 VLOAD VSL*
012348,000226: 10,2264 01521 TDELTAV
012349,000227: 10,2265 57605 0 -7,2
012350,000228: 10,2266 53655 VAD VSL*
012351,000229: 10,2267 01535 RCV
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012353,000231: 10,2270 57576 0,2
012354,000232: 10,2271 25722 STOVL R-OTHER
012355,000233: 10,2272 01527 TNUV
012356,000234: 10,2273 53257 VSL* VAD
012357,000235: 10,2274 57602 0 -4,2
012358,000236: 10,2275 01543 VCV
012359,000237: 10,2276 77657 VSL*
012360,000238: 10,2277 57576 0,2
012361,000239: 10,2300 01730 STORE V-OTHER
012362,000240: 10,2301 77616 RVQ
012363,000241:
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012365,000243: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012366,000244:
012367,000245: # ENTRY: CALL
012368,000246: # LOG
012369,000247:
012370,000248: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012371,000249:
012372,000250: # EBANK IS ARBITRARY..
012373,000251:
012374,000252: 14,2000 BANK 14
012375,000253: 23,2000 SETLOC POWFLIT2
012376,000254: 23,2000 BANK
012377,000255: 23,2155 COUNT 23/GEOM
012378,000256:
012379,000257: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012380,000258: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012381,000259: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012382,000260: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012383,000261: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012384,000262: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012385,000263: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012386,000264: 23,2165 01001 14636 2DEC .031335467
012387,000265: 23,2167 00325 07310 2DEC .0130145859
012388,000266: 23,2171 00541 16735 2DEC .0215738898
012389,000267:
012390,000268: 23,2173 35021 CAF ZERO
012391,000269: 23,2174 54156 TS MPAC +2
012392,000270: 23,2175 00006 EXTEND
012393,000271: 23,2176 32214 DCA CLOG2/32
012394,000272: 23,2177 52155 DXCH MPAC
012395,000273: 23,2200 52160 DXCH MPAC +3
012396,000274: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012397,000275: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012398,000276:
012399,000277: 23,2203 52156 DXCH MPAC +1
012400,000278: 23,2204 52155 DXCH MPAC
012401,000279: 23,2205 52160 DXCH MPAC +3
012402,000280: 23,2206 20155 DAS MPAC
012403,000281: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012404,000282:
012405,000283: 23,2210 77616 RVQ
012406,000284:
012407,000285: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012408,000286:
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012410,000288: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012411,000289:
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012413,000291: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012414,000292: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012415,000293: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012416,000294:
012417,000295: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012418,000296: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012419,000297: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012420,000298: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012421,000299: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012422,000300: # THE EQUATIONS ARE
012423,000301: # - - - -
012424,000302: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012425,000303:
012426,000304: # WHERE WT = WIE DTEAROT
012427,000305:
012428,000306: # RTINIT = INITIAL TARGET VECTOR
012429,000307: # - - -
012430,000308: # RTEAST = UNITW * RTINIT
012431,000309: # - - -
012432,000310: # RTNORM = RTEAST * UNITW
012433,000311:
012434,000312: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012435,000313: #
012436,000314: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012437,000315: # STCALL DTEAROT STCALL DTEAROT
012438,000316: # EARROT1 EARROT2
012439,000317: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012440,000318: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012441,000319:
012442,000320: # SUBROUTINES USED: NONE
012443,000321:
012444,000322: # NORMAL EXIT MODES: RVQ
012445,000323:
012446,000324: # ALARMS: NONE
012447,000325:
012448,000326: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012449,000327: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012450,000328: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012451,000329: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012452,000330:
012453,000331: # ERASABLE INITIALIZATION REQUIRED:
012454,000332: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012455,000333: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012456,000334: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012457,000335:
012458,000336: # DEBRIS: QPRET, PDL+0 ... PDL+5
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012460,000338: 23,2215 E7,1451 EBANK= RTINIT
012461,000339:
012462,000340: 23,2215 47375 EARROT1 VLOAD VXV
012463,000341: 23,2216 01714 UNITW # FULL UNIT VECTOR
012464,000342: 23,2217 03452 RTINIT # .5 UNIT
012465,000343: 23,2220 03460 STORE RTEAST # .5 UNIT
012466,000344:
012467,000345: 23,2221 77635 VXV
012468,000346: 23,2222 01714 UNITW # FULL UNIT
012469,000347: 23,2223 17466 STODL RTNORM # .5 UNIT
012470,000348: 23,2224 03606 DTEAROT # (-28) CS
012471,000349:
012472,000350: 23,2225 56204 EARROT2 BOVB DDV
012473,000351: 23,2226 57352 TCDANZIG # RESET OVFIND, IF ON
012474,000352: 23,2227 06256 1/WIE
012475,000353: 23,2230 41400 BOV PUSH
012476,000354: 23,2231 46245 OVERADAY
012477,000355: 23,2232 45346 COS DSU
012478,000356: 23,2233 15333 HIDPHALF
012479,000357: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012480,000358: 23,2235 03466 RTNORM # .5 UNIT
012481,000359: 23,2236 74356 SIN VXSC
012482,000360: 23,2237 03460 RTEAST # .5 UNIT
012483,000361: 23,2240 76455 VAD VSL1
012484,000362: 23,2241 53455 VAD UNIT # INSURE THAT RT IS 'UNIT'.
012485,000363: 23,2242 03452 RTINIT # .5 UNIT
012486,000364: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012487,000365:
012488,000366: 23,2244 77616 RVQ
012489,000367:
012490,000368: 23,2245 75345 OVERADAY DLOAD SIGN
012491,000369: 23,2246 06256 1/WIE
012492,000370: 23,2247 03606 DTEAROT
012493,000371: 23,2250 77621 BDSU
012494,000372: 23,2251 03606 DTEAROT
012495,000373: 23,2252 03606 STORE DTEAROT
012496,000374:
012497,000375: 23,2253 77650 GOTO
012498,000376: 23,2254 46225 EARROT2
012499,000377:
012500,000378: # WIE 2DEC .1901487997
012501,000379: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012502,000380: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012503,000381: 23,2261 00000 00000 2DEC 0 B-28
012504,000382: 23,2263 67313 65307 2DEC -.5376381241 B-1
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012506,000384: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012507,000385: 23,2267 20000 00000 HALFNFLT 2DEC .5
012508,000386: 23,2271 00000 00000 2DEC 0 B-28
012509,000387: 23,2273 10464 12470 2DEC +.5376381241 B-1
012510,000388: 23,2275 00000 00000 2DEC 0 B-28
012511,000389: 23,2277 15373 11346 2DEC +.8431756920 B-1
012512,000390: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012513,000391: 23,2303 00000 00000 2DEC 0 B-28
012514,000392: 23,2305 10464 12470 2DEC +.5376381241 B-1
012515,000393: 23,2307 00000 00000 2DEC 0 B-28
012516,000394: 23,2311 20000 00000 2DEC .5
012517,000395: 23,2313 00000 00000 2DEC 0 B-28
012518,000396: 23,2315 67313 65307 2DEC -.5376381241 B-1
012519,000397: 23,2317 00000 00000 2DEC 0 B-28
012520,000398: 23,2321 15373 11346 2DEC +.8431756920 B-1
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Page 296
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012522,000400: 23,2323 07020 10DEGS- DEC 3600 B-14
012523,000401: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 2S COMP.
012524,000402: 23,2325 00000 OCT 00000
012525,000403: 23,2326 61740 20DEGS- DEC -07199 B-14
012526,000404: 23,2327 77777 DEC -00000 B-14
012527,000405: 23,2330 07020 20DEG- DEC 03600 B-14
012528,000406: 23,2331 00000 DEC 00000 B-14
012529,000407:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc